DELTA 1 R/B, 2661

Orbit data source: Space-Track

DELTA 1 R/B, 2661 is space debris in SSO originally from a launch on Thu, 26 Jan 1967 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
2661, 1967-006B
Orbit
SSO
Last TLE update
14 hours ago
Origin
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1967-01-26 (58 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 14 hours ago
0 DELTA 1 R/B
1 02661U 67006B   25199.42249512 -.00000053  00000-0 -23612-4 0  9997
2 02661 101.9663 262.7744 0064643 351.1308  19.8063 12.68013275705856
Epoch: 2025-07-18T10:08Z
TLE epoch observation values (Epoch: 2025-07-18T10:08:23.578Z)
Latitude
10.90027°
Longitude
171.87449°
Altitude
1,344.669 km
Speed
7.208 km/s
True Right ascension
17h 21m 47s
True Declination
10° 50' 29"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
76.59452°
Longitude
57.02854°
Altitude
1,416.629 km
Speed
7.153 km/s
Apparent Right ascension
01h 55m 08s
Apparent Declination
42° 30' 41"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:38:02
Azimuth
345.845° N
Elevation
-5.745°
Doppler factor
1
Orbital elements
Apogee altitude
1,437.779 km
Perigee altitude
1,337.38 km
Semi-major axis
7,765.717 km
Eccentricity
0.00646
Inclination
101.9663°
RAAN
262.7744°
Arg. of periapsis
351.1308°
True anomaly
20.05922°
Mean anomaly
19.8063°
Eccentric anomaly
19.93257°
Mean motion
3.17154 °/min
Orbital period
113.51 mins
BSTAR
-0.000023612
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Other satellites on launch #6 in the year 1967 (1967-01-26 UTC)
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